Author:
Angeletti F.,Iannelli P.,Gasbarri P.,Gonzalez J. A. Perez,Ellero N.,Wattrelot T.,Ankersen F.,Sabatini M.,Celani F.,Palmerini G.B.
Reference11 articles.
1. Linear Dynamic Modeling of Spacecraft with Various Flexible Appendages and On-board Angular Momentums;Alazard,2008
2. End-to-end design of a robust attitude control and vibration suppression system for large space smart structures;Angeletti;Acta Astr,2021
3. Robust Attitude Control Design for the BIOMASS Satellite (Earth Explorer Core Mission Candidate);Bennani;IFAC Proc,2011
4. Integrated Design of System Parameters, Control and Sensor Actuator Placement for Symmetric Mechanical Systems;Hiramoto,2009
5. Model-Based FDI Applied to a Piezoelectric Active Vibration Suppression System for Smart Flexible Spacecraft;Iannelli;Aerotec. Missili Spaz.,2021
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